Compressible Flow Pro
Free AppAbout Compressible Flow Pro
Compressible Flows Equations:
1) Isentropic relationships
2) Normal Shock Calculator for aerodynamics compressible flows
3) Oblique Shock
4) Gas properties, more will be added
P0=stagnation pressure, T0=stagnation temperature
Equations:
P0=P*(1+0.5(gamma-1)Mach^2)^(gamma)/(gamma-1)
T0=T*(1+0.5(gamma-1)Mach^2)
For engineering students and/or aerospace engineers; let me know how I can improve this app
The Heat Capacity ratio of the gas can be changed and few references values can be chosen
Disclaimer:
I have checked the equations but it is always possible to have a bug; double check the results
fonts used in the icon Crimson Text: http://aldusleaf.org/index.php
1) Isentropic relationships
2) Normal Shock Calculator for aerodynamics compressible flows
3) Oblique Shock
4) Gas properties, more will be added
P0=stagnation pressure, T0=stagnation temperature
Equations:
P0=P*(1+0.5(gamma-1)Mach^2)^(gamma)/(gamma-1)
T0=T*(1+0.5(gamma-1)Mach^2)
For engineering students and/or aerospace engineers; let me know how I can improve this app
The Heat Capacity ratio of the gas can be changed and few references values can be chosen
Disclaimer:
I have checked the equations but it is always possible to have a bug; double check the results
fonts used in the icon Crimson Text: http://aldusleaf.org/index.php
All Application Badges
Free
downl.
downl.
Android
1.5+
1.5+
Android app
App History & Updates
More downloads Compressible Flow Pro reached 500 - 1 000 downloads
More downloads Compressible Flow Pro reached 100 - 500 downloads
What are users saying about Compressible Flow Pro
M
by M####:
by M####:
Great app. Thanks
Q
by Q####:
by Q####:
I used another app similar to this one but you could add more than one shocks or isentropic flow table and get the results. App can be improved by allowing users to add consecutive shocks.
Y
by Y####:
by Y####:
Great app. Thanks
V
by V####:
by V####:
Consecutive tables I used another app similar to this one but you could add more than one shocks or isentropic flow table and get the results. App can be improved by allowing users to add consecutive shocks.
T
by T####:
by T####:
SGs2 Great app. Thanks
by M####:
Unfortunately the values I found using the oblique shock angles are incorrect. As well as there being limited inputs despite being able to find any one value for two inputs from the governing equations. I did verify the values against tables in "Introduction to Compressible Fluid Flow"